AYAME 1 DEB

NORAD ID: 38682

Int'l Code: 1979-009E

Perigee: 12,625.7 km

Apogee: 34,289.0 km

Inclination: 10.8 °

Period: 854.5 minutes

Semi major axis: 29828 km

RCS: 0.003 m² (small)

Launch date: February 6, 1979
Source: Japan (JPN)
Launch site: TANEGASHIMA SPACE CENTER (TNSTA)

Note: This is SATELLITE DEBRIS

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Two Line Element Set (TLE):

1 38682U 79009E   23337.95350834 -.00000127  00000-0  00000+0 0  9997
2 38682  10.7518 351.9194 3631337  37.3292 343.2317  1.68522864 95127

Source of the keplerian elements: AFSPC